• Title/Summary/Keyword: 분무침투깊이

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A numerical study on the characteristics of internal flows in a gasoline direct swirl injector (직접분사식 가솔린 선회 분사기에서의 내부 유동특성에 관한 수치 해석)

  • Bae, S.H.;Moon, S.Y.;Lee, C.W.
    • Journal of ILASS-Korea
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    • v.6 no.2
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    • pp.9-15
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    • 2001
  • The internal flow characteristics of a gasoline direct injector have been studied to improve fuel economy and reduce exhaust emissions. Computational Fluid Dynamics (CFD) is used to examine the internal flow of the GDI with the purpose of designing the optimum geometry of the injector. This study tests orifice length, cone angle, swirl angle, orifice diameter and needle lift. The results show that optimum sizes of the orifice length, cone angle, swirl angle, orifice diameter and needle lift are 0.8mm, $140^{\circ},\;120^{\circ},\;80mm\;and\;70{\mu}m$, respectively. The size of the lift does not affect the formation of the air core signficantly near the tip of the needle compared to the ball-type needle. The vena contracta phenomenon near the orifice inlet can be released by smoothing the edge.

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An experimental study for the prediction of combustion performance of the Unlike Impinging Quadlet Injector (충돌형 Quadlet 인젝터의 연소성능 예측에 관한 실험적 연구)

  • Kim, J.W.;Park, H.H.;Han, J.S.;Kim, S.J.;Kim, Y.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.4
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    • pp.44-50
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    • 1999
  • For the prediction of combustion performance of the Unlike Impinging Quadlet Injector (OOOF type), mixing efficiency, mixing characteristic velocity, and efficiency of mixing characteristic velocity were obtained from the cold test. Water/kerosene were used for simulants, The momentum ratio of oxidizer and fuel were mixing correlating parameter. Orifice discharge coefficient, spray pattern and mass distribution were measured. As a result, invasion-depth had strong effect on mixing efficiency, mixing characteristic velocity, and efficiency of mixing characteristic velocity. Mixing efficiency and efficiency of mixing characteristic velocity showed maximum value for momentum ratio 1.67(TMR = 2.5), and fuel rich state showed larger decreasing ratio than oxidizer rich state.

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